JPS6399123A - Reamer - Google Patents

Reamer

Info

Publication number
JPS6399123A
JPS6399123A JP24586786A JP24586786A JPS6399123A JP S6399123 A JPS6399123 A JP S6399123A JP 24586786 A JP24586786 A JP 24586786A JP 24586786 A JP24586786 A JP 24586786A JP S6399123 A JPS6399123 A JP S6399123A
Authority
JP
Japan
Prior art keywords
drill
cutting edge
reamer
straight line
diameter
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP24586786A
Other languages
Japanese (ja)
Other versions
JPH0523886B2 (en
Inventor
Koichiro Wakihira
脇平 浩一郎
Michitaka Katsuta
勝田 通隆
Masayasu Hino
日野 正保
Tomokichi Kosaka
小坂 友吉
Toshio Sasayama
笹山 敏男
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Kobe Steel Ltd
Original Assignee
Kobe Steel Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Kobe Steel Ltd filed Critical Kobe Steel Ltd
Priority to JP24586786A priority Critical patent/JPS6399123A/en
Publication of JPS6399123A publication Critical patent/JPS6399123A/en
Publication of JPH0523886B2 publication Critical patent/JPH0523886B2/ja
Granted legal-status Critical Current

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  • Drilling Tools (AREA)
  • Milling, Broaching, Filing, Reaming, And Others (AREA)

Abstract

PURPOSE:To make is possible to prevent a drill section from being broken, by forming cutting edges formed in grooves and chisel cutting edges formed in a thick core part by thinning in straight line-like shapes, respectively, and by setting the angle of the cutting edge to a value less than a predetermined angle. CONSTITUTION:Cutting edges 4 formed in grooves 3 are formed in a straight-line L shape so as to extend from a point P0 on the outermost periphery to the center axis O, and the centriperal angle alpha of the cutting edges 4 which respect to the straight- line L is set within a range of + or -5 deg.. Further, chisel cutting edges 7 formed by parts 6 which are ground off by thinning are formed in a straight line-like shape, extending from a point Pi on the innermost periphery to the center axis O with the axial rake angle theta thereof being set within a range of + or -5 deg.. Further, the diameter C of the thick core part 1 is set within a range of 0.25-0.4 times large as the diameter D of the drill part, and a remaining core part which is formed when a chisel point 8 is left without being ground during thinning, is set within a range of 0-0.1 times as large as the diameter D of the drill part. Thus, it is possible to obtain a strength sufficient for preventing the drill part from being broken, and to facilitate the regrinding process.

Description

【発明の詳細な説明】[Detailed description of the invention] 【産業上の利用分野】[Industrial application field]

本発明は、ドリル部を有するリーマに係り、特に、その
ドリル部の切刃が再研削作業の容易な切刃形状を有する
リーマに関するものである。
The present invention relates to a reamer having a drill portion, and particularly to a reamer in which the cutting edge of the drill portion has a cutting edge shape that facilitates re-grinding.

【従来技術】[Prior art]

従来の穴あけ加工では、ドリルで下穴を穿孔加工した後
にリーマで仕上げ加工を行なっている。 しかしながら、この工程ではドリルおよびリーマの2種
類の工具を使用するので、作業時間が長くなり、工具費
用も大きくなるという問題があった。 この問題を解決するものとして、第5図に示すように、
上記下穴の穿孔加工を行なうドリル部5と仕上げ加工を
行なうリーマ部lOとが一体に構成されたリーマ11が
開発されている。このリーマ11によれば、上記二種類
の加工を一つの工具で行なうことができ、加工時間が短
縮されるとともに工具費用の軽減も達成しうろ。
In conventional drilling, a pilot hole is drilled using a drill, and then finishing is performed using a reamer. However, since two types of tools, a drill and a reamer, are used in this process, there are problems in that the working time is long and the tool cost is also high. As a solution to this problem, as shown in Figure 5,
A reamer 11 has been developed in which a drill part 5 for drilling the pilot hole and a reamer part 10 for finishing the hole are integrated. According to this reamer 11, the above-mentioned two types of machining can be performed with one tool, thereby reducing machining time and tool costs.

【発明が解決しようとする問題点】[Problems to be solved by the invention]

ところで、一般に切削工具にあっては、材質の剛性およ
び脆性と切削抵抗との相対的な関係に基づいて生じる切
損や切刃のチッピングの問題がある。上述のようなり−
マにおいてら、ドリル部5の切刃のチッピングは下穴の
精度を損ない、ひいてはリーマ部10による仕上げ加工
の精度にも影響を及ぼす結果になる。 例えば、ドリルに関しては、特公昭61−30845号
公報や特公昭58−18163号公報に、切削抵抗を小
さくして切刃のチッピングを防止するために、切刃のl
:j、i面直視形状をそれぞれ特定の曲線により形成す
る技術が開示されているが、これら曲線によって切刃か
形成されたドリルにあっても、その寿命のばらつきは大
きく、その主要原因はチッピングにあると考えられろ。 このチッピングが生じる原因の一つは、切刃が湾曲して
いることに起因しており、この切刃が湾曲していると切
刃に微小面取りを施すホーニング加工が難しく、従来て
はノ\ンドラッパと呼ばれる工具を用いろ手作業によっ
てそのホーニング加工が行なわれていたが、切刃が湾曲
しているとその仕上がり精度は作業者の熟練度に依存す
る度合が大きく、その結果仕上がり精度の“ばらつき”
が生じている。したがって、切削性能が安定仕す、また
、寿命の“ばらつき”を生じる原因ともなっている。 特にトリルの場合には、切刃にチッピングが生じるとこ
れを再研削によって再生して用いるが、切刃を精密な曲
線形状に仕上げることは極めて高度な技術を要する。特
に中心部の切刃すなわちヂゼル刃が湾曲形状に形成され
ていては刃立研削が難しく、特別な専用工作機械が必要
となる。 まf二、ヂゼル刃とその外周側に連続してd?を部に延
在する切刃との連続部分における形状が滑らかに変化し
ていないため、この部分に切削抵抗か集中してデツピン
グが生じやすい。 本発明は上述のごとき問題点に鑑み、これらを有効に解
決すべく創案されたものである。したがってその目的は
、一般の工具鋼製の場合は勿論、超硬合金製の場合であ
っても、ドリル部の切損を十分に防止しうる強度と、ド
リル部の切刃の十分な切れ味と、切刃のホーニング加工
および再研削加工が容易であり且つデツピングの生じに
くい切刃形状のドリル部を備えて仕上げ精度の高いリー
マを提供することにある。
By the way, cutting tools generally have the problem of cutting damage and chipping of the cutting edge, which occur based on the relative relationship between the rigidity and brittleness of the material and the cutting resistance. As mentioned above-
In the reamer, chipping of the cutting edge of the drill section 5 impairs the precision of the prepared hole, and in turn affects the precision of finishing by the reamer section 10. For example, regarding drills, in Japanese Patent Publication No. 61-30845 and Japanese Patent Publication No. 58-18163, in order to reduce cutting resistance and prevent chipping of the cutting edge,
: A technology has been disclosed in which the direct view shape of the j and i planes is formed using specific curves, but even with drills whose cutting edges are formed according to these curves, the lifespan of the drills varies widely, and the main cause of this is chipping. It is thought that there is. One of the causes of this chipping is that the cutting edge is curved, and when the cutting edge is curved, it is difficult to perform honing, which is the process of applying a minute chamfer to the cutting edge. The honing process was done manually using a tool called a drapper, but if the cutting edge is curved, the accuracy of the finished product is highly dependent on the skill level of the operator, and as a result, the accuracy of the finished product is scattering"
is occurring. Therefore, cutting performance is not stable, and it is also a cause of "variation" in life. Particularly in the case of trills, if chipping occurs on the cutting edge, it is re-grinded and reused, but finishing the cutting edge into a precise curved shape requires extremely advanced technology. In particular, if the cutting edge at the center, that is, the diesel blade, is formed into a curved shape, edge grinding is difficult, and a special dedicated machine tool is required. Ma f2, d continuously on the zizel blade and its outer circumference side? Since the shape of the continuous part with the cutting edge that extends to the part does not change smoothly, the cutting force is concentrated in this part and depping is likely to occur. The present invention has been devised in view of the above problems and to effectively solve them. Therefore, the purpose of this tool is to provide sufficient strength to prevent the drill part from breaking and to provide sufficient sharpness to the cutting edge of the drill part, whether it is made of general tool steel or cemented carbide. Another object of the present invention is to provide a reamer with high finishing accuracy, which is equipped with a drill portion having a cutting edge shape that allows easy honing and re-grinding of the cutting edge and prevents depping.

【問題点を解決するための手段】[Means to solve the problem]

本発明に係るリーマは、従来技術の問題点を解決し、目
的を達成するために以下のような構成を備えている。 すなわち、リーマ部の先端にドリル部を形成してなるリ
ーマにおいて、ド1ノル部の軸方向端面に形成される切
刃の端面直視形状に関して、溝部に形成される切刃と、
心厚部にシンニングによって形成されるヂゼル刃とがそ
れぞれ直線状に形成されている。切刃の最外周端の点と
ドリル部の軸心とを通る直線に対して、切刃の直線がな
す角は該リーマの回転方向ヘ−5°以上+5°以下であ
る。 心厚部の直径寸法はドリル部直径の0.25倍以」−0
、4倍以下である。チゼル刃は、その軸方向す(い角が
一5°以上+5°以下であり、且つその先端心残し寸法
は、ドリル直径の0倍以上0.1倍以下である。 なお、本発明のり−マは、一般の工具鋼製り−マにおい
ても十分有効であるが、特にリーマを超硬合金で製作す
る場合には、その材質の脆さを克服する技術として甚だ
有効である。
The reamer according to the present invention has the following configuration in order to solve the problems of the prior art and achieve the purpose. That is, in a reamer in which a drill part is formed at the tip of the reamer part, with respect to the shape of the cutting edge formed on the axial end face of the drill part when viewed directly from the end surface, the cutting edge formed in the groove part,
Diesel blades formed by thinning in the thick core portion are each formed in a straight line. The angle formed by the straight line of the cutting blade with respect to the straight line passing through the outermost point of the cutting blade and the axis of the drill part is -5° or more and +5° or less in the rotational direction of the reamer. The diameter of the thick core part is 0.25 times or more the diameter of the drill part"-0
, is 4 times or less. The chisel blade has an axial angle of 15° or more and +5° or less, and its tip center remaining dimension is 0 times or more and 0.1 times or less of the drill diameter. Although the reamer is sufficiently effective in general tool steel reamers, it is particularly effective when the reamer is made of cemented carbide as a technique for overcoming the brittleness of that material.

【作用] 本発明に係るドリルは、従来技術の問題点を解決し、目
的を達成するために以下のように作用する。 すなわち、ドリル部の軸方向端面に形成される切刃の端
面直視形状に関して、溝部に形成される切刃と、心厚部
にシンニングによって形成されるヂゼル刃とがそれぞれ
直線状に形成されているので、切刃のホーニング加工お
よび再研削加工が工具を直線的に移動させるだけの操作
によって行なえ、かつ切削抵抗が一箇所に集中すること
がなく切刃全体にわたって略均等に分散される。 切刃の最外周端の点とドリル部の軸心とを通る直線に対
して、切刃の直線がなす角をリーマの回転方向ヘ−5°
以上+5°以下とすることによつて、切刃の径方向のす
くい角が所定の範囲内に抑えられるので、切削抵抗も小
さく抑えられ、切刃の十分な切れ味が確保される。 心厚部の直径寸法がドリル部直径の0.25倍以上0.
4倍以下で十分に大きくされているので、ドリル部の曲
げ剛性および捩れ剛性が高められ、特に超硬合金等の脆
い材質により製造されろ場合の切損を防止し、重切削を
も可能ならしめる。 ヂゼル刃は、その軸方向すくい角を一5°以上+5°以
下とすることによって、ヂゼル刃の強度を損なわずにそ
の切れ味が確保される。また、ドリル部直径の0倍以上
0.1倍以下の先端心残し寸法の心残し部を形成するこ
とによって、チゼル刃先端の必要な強度、すなわち切削
条件に応じてヂゼルポイントの圧壊を防止しうろ強度が
確保され、さらにはドリル部の食いつき性を高めて先端
の歩行現象をなくし、心のずれをなくす。すなわち、ド
リル部によって所定の位置で精度よく穴あけが行なえる
ため、その後にリーマ部がその下穴の内周面を切削する
際に、リーマ部の各切刃がバランス良く切削を行なうこ
とができ、リーマ部による仕上げ精度ら向上する。 【実施例】 以下に本発明の好適一実施例について第1図ないし第4
図を参照して説明する。 第1図は本発明に係るリーマのドリル部の切刃を端面側
から直視して示す平面図である。 図中lは心厚部、2はランド部、3は溝部である。′f
!部3に形成される切刃4の直線もしくは曲線は、ドリ
ル部5の直径、捩れ角、心厚および先端角によって決定
されるが、本実施例のり−マ11のドリル部5の切刃4
は、その最外周端の点Poからドリル5の軸心Oに向か
って直線状に形成されている。すなわち、切刃4の最外
周端の点Poと軸心Oとを通る直ILに対して、切刃4
の直線かリーマ11の回転方向(図中矢印Aで示す)へ
なす角αを同心度と定義すると、本実施例では同心度が
0°に設定されている。しかし、本発明のり−マはこれ
に限定されるものではなく、第2図または第3図示に示
すように、ドリル部5の切刃4の同心度が±5°の範囲
内で設定されていればよい。 スマッジングで示す部分6はシンニングによって削り落
とされた部分であり、7はこのシンニングによって形成
されたチゼル刃である。このヂゼル刃7も切刃4の最内
周端の点Piから軸心Oに向かって直線状に形成されて
いる。 心厚部Iの直径寸法Cは、ドリル部直径りの0.25倍
以上0.4倍以下の範囲内に設定されている。 第4図は、第1図のIV−IV線矢視断面図であるが、
チゼル刃7の軸方向のすくい角θは一5°以上+5°以
下の範囲内に設定されている。 if図ないし第3図に図示した実施例では、シンニング
時にチゼルポイント部8を削り残して形成される心残し
部の寸法が0であるが、切削条件に応じてヂゼルポイン
ト部8の圧壊を防止できろ剛性を持たせるため、ドリル
部直径りの0倍以上0.1倍以下の範囲内でその心残し
部が形成されてもよい。 なお、ドリル部5の軸心Oに対して点対称な直線切刃4
,7によって削り出される切り屑は、外周部で削り出さ
れる切り屑と内周部で削り出される切り屑との周速差が
大きいためブレイクされやすく、切り屑の排出性を高め
る。
[Function] The drill according to the present invention functions as follows in order to solve the problems of the prior art and achieve the purpose. That is, regarding the shape of the cutting edge formed on the axial end surface of the drill portion when viewed directly from the end surface, the cutting edge formed in the groove portion and the diesel edge formed in the thick core portion by thinning are each formed in a straight line. Therefore, honing and re-grinding of the cutting edge can be performed by simply moving the tool linearly, and the cutting resistance is not concentrated in one place but is distributed approximately evenly over the entire cutting edge. The angle formed by the straight line of the cutting blade with the straight line passing through the outermost point of the cutting blade and the axis of the drill part is -5° in the rotation direction of the reamer.
By setting the angle to +5° or less, the rake angle in the radial direction of the cutting blade is suppressed within a predetermined range, so the cutting resistance is also suppressed to a small level, and sufficient sharpness of the cutting blade is ensured. The diameter of the thick core part is 0.25 times or more the diameter of the drill part.
Since it is sufficiently large (less than 4 times), the bending and torsional rigidity of the drill part is increased, and it prevents breakage especially when manufactured from brittle materials such as cemented carbide, and allows heavy cutting. Close. By setting the axial rake angle of the diesel blade to 15 degrees or more and +5 degrees or less, the sharpness of the diesel blade is ensured without impairing its strength. In addition, by forming a centering portion with a tip centering dimension of 0 times to 0.1 times the diameter of the drill part, the required strength of the chisel blade tip, that is, the crushing of the chisel point can be prevented depending on the cutting conditions. Strength is ensured, and the biting ability of the drill part is improved to eliminate the walking phenomenon of the tip and to eliminate misalignment of the center of the drill. In other words, since the drill part can accurately drill a hole at a predetermined position, when the reamer part cuts the inner circumferential surface of the prepared hole, each cutting edge of the reamer part can cut in a well-balanced manner. , the finishing accuracy of the reamer section is improved. [Example] A preferred embodiment of the present invention will be described below with reference to Figures 1 to 4.
This will be explained with reference to the figures. FIG. 1 is a plan view showing the cutting edge of the drill portion of the reamer according to the present invention, viewed directly from the end surface side. In the figure, 1 is a core thick part, 2 is a land part, and 3 is a groove part. 'f
! The straight line or curve of the cutting edge 4 formed in the section 3 is determined by the diameter, helix angle, core thickness, and tip angle of the drill section 5.
is formed in a straight line from the outermost point Po toward the axis O of the drill 5. That is, the cutting edge 4 is
If the angle α between the straight line and the rotational direction of the reamer 11 (indicated by arrow A in the figure) is defined as concentricity, then in this embodiment, concentricity is set to 0°. However, the lamer of the present invention is not limited to this, and as shown in FIG. 2 or 3, the concentricity of the cutting edge 4 of the drill portion 5 is set within a range of ±5°. That's fine. A portion 6 shown by smudging is a portion shaved off by thinning, and 7 is a chisel blade formed by this thinning. This diesel blade 7 is also formed in a straight line from a point Pi at the innermost peripheral end of the cutting blade 4 toward the axis O. The diameter dimension C of the core thick part I is set within a range of 0.25 times or more and 0.4 times or less of the diameter of the drill part. FIG. 4 is a sectional view taken along the line IV-IV in FIG.
The rake angle θ of the chisel blade 7 in the axial direction is set within a range of -5° or more and +5° or less. In the embodiments shown in FIGS. IF to 3, the dimension of the centering part formed by leaving the chisel point part 8 uncut during thinning is 0, but crushing of the chisel point part 8 can be prevented depending on the cutting conditions. In order to provide rigidity, the center portion may be formed within a range of 0 times or more and 0.1 times or less the diameter of the drill portion. Note that the straight cutting edge 4 is point symmetrical with respect to the axis O of the drill part 5.
, 7 are easily broken due to the large circumferential speed difference between the chips cut out at the outer circumference and the chips cut out at the inner circumference, improving the evacuation of the chips.

【発明の効果】【Effect of the invention】

以上の説明より明らかなように、本発明によれば次のご
とき優れた効果が発揮される。 すなわち、ドリル部の切刃が略−直線に形成されるので
そのホーニング加工が容易であり、加工精度の“ばらつ
き”も少なくなって工具寿命が平均化され、極端に寿命
の短いものがなくなる。また、再研削も容易に行なえ、
ユーザーが行なうことも可能となる。さらに、チッピン
グの生じやすい箇所がなくなるので全体にデツピング発
生率が低くなり、工具寿命は長くなる。心厚は十分に確
保されているのでドリル部の切損を十分に防止できる。 また、ドリル部切刃の同心度を所定の範囲内に設定する
ことによって、切刃の径方向のすくい角も所定の範囲内
に抑えられるので、切削抵抗ち小さく抑えられ、切刃の
十分な切れ味が確保される。 心厚が十分に確保されているので、ドリル部の切損を防
止しうる。 チゼル刃には適切な軸方向すくい角が付与されているの
で、強度を損なわずにその切れ味が確保される。 先端心残し部が必要に応じた寸法で形成されるので、チ
ゼル刃先端の必要な強度が確保され、さらにはドリル部
の食いつき性を高めて先端の歩行現象をなくし、心のず
れをなくす。すなわち、ドリル部によって所定の位置で
精度よく穴あけが行なえるため、その後にリーマ部がそ
の下穴の内周面を切削する際に、リーマ部の各切刃がバ
ランス良く切削を行なうことができ、リーマ部による佳
上げ精度ら向上する。
As is clear from the above description, the present invention provides the following excellent effects. That is, since the cutting edge of the drill portion is formed substantially straight, it is easy to honing it, and "variations" in machining accuracy are reduced, so that the tool life is averaged and there are no tools that have an extremely short life. Also, re-grinding can be done easily.
This can also be done by the user. Furthermore, since there are no locations where chipping is likely to occur, the overall incidence of chipping is lowered and the tool life is extended. Since the core thickness is sufficiently ensured, breakage of the drill part can be sufficiently prevented. In addition, by setting the concentricity of the cutting edge of the drill part within a predetermined range, the rake angle in the radial direction of the cutting edge can also be suppressed within a predetermined range, so cutting resistance can be kept small and the cutting edge can be fully Sharpness is ensured. Since the core thickness is sufficiently ensured, breakage of the drill part can be prevented. The chisel blade has an appropriate axial rake angle, ensuring sharpness without sacrificing strength. Since the tip center remaining portion is formed with the necessary dimensions, the necessary strength of the chisel blade tip is ensured, and furthermore, the biting property of the drill part is improved to eliminate the tip walking phenomenon and center misalignment. In other words, since the drill part can accurately drill a hole at a predetermined position, when the reamer part cuts the inner circumferential surface of the prepared hole, each cutting edge of the reamer part can cut in a well-balanced manner. , the lifting accuracy of the reamer section is improved.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本発明に係るリーマの一実施例において、その
ドリル部の切刃を端面側から直視して示す平面図である
。第2図および第3図は、それぞれ本発明に係るリーマ
の他の一実施例において、そのドリル部の切刃を端面側
から直視して示す平面図である。第4図は第1図のIV
−I’/徨矢視断面図である。第5図はリーマ部の先端
にドリル部を有するリーマの一般的概略構成を示す正面
図である。 l・・・心厚部、4・・・切刃、5・・・ドリル部、7
・・・チゼル刃、10・・・リーマ部、C・・・心厚部
の直径寸法、D・・・ドリル部直径、Po・・・切刃の
最外周端の点、0・・・ドリルの軸心、L・・・点PO
と軸心0を通る直線、α・・・直線りに対して切刃の直
線がドリルの回転方向へなす角、0・・・チゼル刃の軸
方向のすくい角。
FIG. 1 is a plan view showing the cutting edge of the drill portion of an embodiment of the reamer according to the present invention, viewed directly from the end surface side. FIGS. 2 and 3 are plan views showing the cutting edge of the drill portion of another embodiment of the reamer according to the present invention, viewed directly from the end surface side. Figure 4 is the IV of Figure 1.
-I'/It is a sectional view taken along the arrow. FIG. 5 is a front view showing a general schematic configuration of a reamer having a drill portion at the tip of the reamer portion. l... Thick core part, 4... Cutting edge, 5... Drill part, 7
...Chisel blade, 10...Reamer part, C...Diameter of thick core part, D...Drill part diameter, Po...Outermost point of cutting edge, 0...Drill Axis center, L...point PO
and a straight line passing through the axis 0, α...The angle that the straight line of the cutting edge makes in the direction of rotation of the drill with respect to the straight line, 0...The rake angle of the chisel blade in the axial direction.

Claims (1)

【特許請求の範囲】[Claims] (1)、リーマ部(10)の先端にドリル部(5)を形
成してなるリーマにおいて、 前記ドリル部(5)が、 軸方向端面に形成される切刃の端面直視形状に関して、
溝部に形成される切刃(4)と、心厚部(1)にシンニ
ングによって形成されるチゼル刃(7)とがそれぞれ直
線状に形成され、 前記切刃(4)の最外周端の点(Po)と当該ドリル部
(5)の軸心(0)とを通る直線(L)に対して、該切
刃(4)の直線がなす角(α)は該リーマの回転方向ヘ
−5°以上+5°以下であり、 前記心厚部(1)の直径寸法(C)は、前記ドリル部(
5)の直径(D)の0.25倍以上0.4倍以下であり
、前記チゼル刃(7)は、その軸方向すくい角(θ)が
−5°以上+5°以下であり、且つその先端心残し寸法
は、前記ドリル部直径(D)の0倍以上0.1倍以下で
あることを特徴とするリーマ。
(1) In a reamer in which a drill part (5) is formed at the tip of the reamer part (10), the drill part (5) has the following features regarding the shape of the cutting edge formed on the axial end face when viewed directly from the end face.
A cutting edge (4) formed in the groove portion and a chisel blade (7) formed in the thick core portion (1) by thinning are each formed in a straight line, and the outermost peripheral end point of the cutting edge (4) is formed in a straight line. (Po) and the straight line (L) passing through the axis (0) of the drill part (5), the angle (α) formed by the straight line of the cutting edge (4) is −5 in the rotational direction of the reamer. The diameter dimension (C) of the thick core portion (1) is at least +5°, and the diameter dimension (C) of the thick core portion (1) is
5), and the chisel blade (7) has an axial rake angle (θ) of -5° or more and +5° or less, and A reamer characterized in that a tip center remaining dimension is 0 times or more and 0.1 times or less of the drill portion diameter (D).
JP24586786A 1986-10-15 1986-10-15 Reamer Granted JPS6399123A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP24586786A JPS6399123A (en) 1986-10-15 1986-10-15 Reamer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP24586786A JPS6399123A (en) 1986-10-15 1986-10-15 Reamer

Publications (2)

Publication Number Publication Date
JPS6399123A true JPS6399123A (en) 1988-04-30
JPH0523886B2 JPH0523886B2 (en) 1993-04-06

Family

ID=17139996

Family Applications (1)

Application Number Title Priority Date Filing Date
JP24586786A Granted JPS6399123A (en) 1986-10-15 1986-10-15 Reamer

Country Status (1)

Country Link
JP (1) JPS6399123A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2003534927A (en) * 2000-06-02 2003-11-25 ケンナメタル インコーポレイテッド Drill bit for spiral drill and method for forming a cutting groove in drill bit area for spiral drill
US9199315B2 (en) 2000-06-02 2015-12-01 Kennametal Inc. Twist drill and method for producing a twist drill which method includes forming a flute of a twist drill
US10471521B2 (en) 2010-04-27 2019-11-12 Sandvik Intellectual Property Ab Twist drill for advanced materials

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2003534927A (en) * 2000-06-02 2003-11-25 ケンナメタル インコーポレイテッド Drill bit for spiral drill and method for forming a cutting groove in drill bit area for spiral drill
US9199315B2 (en) 2000-06-02 2015-12-01 Kennametal Inc. Twist drill and method for producing a twist drill which method includes forming a flute of a twist drill
US10471521B2 (en) 2010-04-27 2019-11-12 Sandvik Intellectual Property Ab Twist drill for advanced materials

Also Published As

Publication number Publication date
JPH0523886B2 (en) 1993-04-06

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